FIELD: physics, instrument engineering.
SUBSTANCE: invention relates to manufacturing of the aircraft fuselage. The limiting system is made to cooperate with the device sectors for the fuselage manufacturing in which the hub for lamination is limited by the outer surface. The hub contains many movable sectors with the angularl spacing around the axis. Herewith the limiting system is located between each single sector and its adjacent sectors. The system contains the first and the second gripping element held by the first and the second adjacent sectors respectively. The first and the second gripping elements are arranged so that when they are connected to each other, a determined spatial arrangement is formed relative to the second adjacent sector preventing thereby a translational mode along the two directions.
EFFECT: invention provides a combination of the two sectors so that there is the prevention of any relative movement between the sectors at the time of manufacture.
4 cl, 6 dwg
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